Robust H∞/PI state feedback control for aeroengine

Xi Wang; Nai Xiang Han; Xi Fa Li; Yun Hua Li

Robust H_∞/PI state feedback control for aeroengine

Xi Wang^*
, Nai Xiang Han
, Xi Fa Li
, Yun Hua Li

^*此作品的通讯作者

自动化科学与电气工程学院

Beihang University
First Inst. of Air Force

科研成果: 期刊稿件 › 文章 › 同行评审

6 引用（Scopus）

摘要

Considering the uncertainty model of aeroengine, the equivalent certainty system that quadratically stabilizes the plant can be obtained by restricting the H infinity norm of closed loop transform function from the disturbance input to the controlled output. A design method of robust H_∞/PI style controller was given by means of two free parameter in H_∞ state feedback controller subject to the constraints of PI structure. The robust performance was simulated on the SIMULINK environment.

源语言	英语
页（从-至）	364-367
页数	4
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	24
期	4
出版状态	已出版 - 8月 2003

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链接到 Scopus 的出版物

引用此

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title = "Robust H∞/PI state feedback control for aeroengine",

abstract = "Considering the uncertainty model of aeroengine, the equivalent certainty system that quadratically stabilizes the plant can be obtained by restricting the H infinity norm of closed loop transform function from the disturbance input to the controlled output. A design method of robust H∞/PI style controller was given by means of two free parameter in H∞ state feedback controller subject to the constraints of PI structure. The robust performance was simulated on the SIMULINK environment.",

keywords = "Aircraft engine, Controller, Flight control, State feedback",

author = "Xi Wang and Han, \{Nai Xiang\} and Li, \{Xi Fa\} and Li, \{Yun Hua\}",

year = "2003",

month = aug,

language = "英语",

volume = "24",

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journal = "Tuijin Jishu/Journal of Propulsion Technology",

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T1 - Robust H∞/PI state feedback control for aeroengine

AU - Wang, Xi

AU - Han, Nai Xiang

AU - Li, Xi Fa

AU - Li, Yun Hua

PY - 2003/8

Y1 - 2003/8

N2 - Considering the uncertainty model of aeroengine, the equivalent certainty system that quadratically stabilizes the plant can be obtained by restricting the H infinity norm of closed loop transform function from the disturbance input to the controlled output. A design method of robust H∞/PI style controller was given by means of two free parameter in H∞ state feedback controller subject to the constraints of PI structure. The robust performance was simulated on the SIMULINK environment.

AB - Considering the uncertainty model of aeroengine, the equivalent certainty system that quadratically stabilizes the plant can be obtained by restricting the H infinity norm of closed loop transform function from the disturbance input to the controlled output. A design method of robust H∞/PI style controller was given by means of two free parameter in H∞ state feedback controller subject to the constraints of PI structure. The robust performance was simulated on the SIMULINK environment.

KW - Aircraft engine

KW - Controller

KW - Flight control

KW - State feedback

UR - https://www.scopus.com/pages/publications/0346148133

M3 - 文章

AN - SCOPUS:0346148133

SN - 1001-4055

VL - 24

SP - 364

EP - 367

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 4

ER -

Robust H∞/PI state feedback control for aeroengine

摘要

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Robust H_∞/PI state feedback control for aeroengine